Modeling and stability assessment of permanent magnet machine-based DC electrical power system in more electric aircraft
Author:
Publisher
Springer Science and Business Media LLC
Subject
Applied Mathematics,Electrical and Electronic Engineering
Link
https://link.springer.com/content/pdf/10.1007/s00202-023-01863-x.pdf
Reference27 articles.
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2. Areerak K-N, Wu T, Bozhko SV, Asher GM, Thomas DWP (2011) Aircraft power system stability study including effect of voltage control and actuators dynamic. IEEE Trans Aerosp Electron Syst 47:2574–2589. https://doi.org/10.1109/TAES.2011.6034652
3. Areerak K-N, Wu T, Bozhko SV, Asher GM, Thomas DWP (2012) Stability study for a hybrid AC-DC more-electric aircraft power system. IEEE Trans Aerosp Electron Syst 48:329–347. https://doi.org/10.1109/TAES.2012.6129639
4. Wheeler P, Bozhko SV (2014) The more electric aircraft: technology and challenge. IEEE Electrif Mag 2:6–12. https://doi.org/10.1109/MELE.2014.2360720
5. Gao F, Bozhko S, Asher G, Wheeler P, Patel C (2016) An improved voltage compensation approach in a droop-controlled DC power system for the more electric aircraft. IEEE Trans Power Electron 31:7369–7383. https://doi.org/10.1109/TPEL.2015.2510285
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